Lockheed U-2 vs. Douglas C-54 Skymaster
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Lockheed U-2 |
versus |
Douglas C-54 Skymaster |
19.2 m |
63 ft 0 in |
length |
28.60 m |
93 ft 10 in |
4.8 m |
15 ft 9 in |
height |
8.38 m |
27 ft 6 in |
32 m |
105 ft |
wingspan |
35.81 m |
117 ft 6 in |
1 × General Electric F118-101 |
engines |
4 x Pratt & Whitney R-2000 Twin Wasp radial engines |
17,000 lbf (76 kN) |
thrust per engine |
1,200 to 1,450 horsepower (895 to 1,080 kW) |
17,000 lbf (76 kN) |
total thrust |
4,800 to 5,800 horsepower |
18,144 kg |
40,000 lb |
MTOW |
29,484 kg |
65,000 lb |
6,090 nm |
11,278 km |
range |
6,500 km |
3,510 nm |
475 mph |
764 km/h |
cruise speed |
340 km/h |
211 mph |
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capacity |
Up to 50 passengers or 28,500 lb cargo |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.